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时间:2011-04-12 10:07来源:蓝天飞行翻译 作者:航空
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STRUT PRESSURE GAGE ASSEMBLY
A
SHOCK STRUT
SHOCK STRUT OUTBOARD DOOR FITTING UPPER TORSION LINK LOWER SIDE STRUT
STRUT SIDE LOWER SPINDLE
SHOCK STRUT
FWD
TRUCK
MECHANICAL
LOCK

SIDE STRUT LOWER SPINDLE ASSEMBLY
B
DRAG BRACE
SHOCK STRUT OUTBOARD DOOR FITTING C Wing Gear - Component Location (Details from Sht 1) Figure 102 (Sheet 2)
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 32-11-00
 ALL  ú ú 01 Page 103 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL
TRUNNION 
FORK 
TRUNNION 
(REF) 
FWD 
DRAG BRACE 
TRUNNION FORK 

DRAG 
LOWER  BRACE 
SIDE 
STRUT 
UPLOCK 
ROLLER 

INBD FWD
UPLOCK ROLLER
E

Wing Gear - Component Location (Details From Sht 1)
Figure 102 (Sheet 3)

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 ALL  ú ú 01 Page 104 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 FAULT ISOLATION/MAINT MANUAL

SHOCK STRUT CHARGING VALVE SEALS


TRUCK SHIELD AND TRUCK BUMPER


Wing Gear - Component Location (Details From Sht 1)

Figure 102 (Sheet 4)

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 ALL  ú ú 01 Page 105 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
FAULT ISOLATION/MAINT MANUAL

WING GEAR 
WHEEL WELL 
SEE  H 
UPPER 
SIDE STRUT  DOWNLOCK 
BUNGEE 
(REF) 
JURY STRUT 
WING GEAR 
SUPPORT BEAM 
(REF) 
DOWNLOCK 
ACTUATOR 
(REF) 

LOWER SIDE STRUT
TRUCK POSITIONING PRESSURE REDUCING VALVE
FWD
SIDE STRUT
TRUCK POSITIONING PRESSURE REDUCING VALVE
COMPONENT ASSEMBLY H I FROM SHT 1
Wing Gear - Component Location
Figure 102 (Sheet 5)

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 ALL  ú ú 01 Page 106 ú Oct 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 WING LANDING GEAR - REMOVAL/INSTALLATION
________________________________________
 1.  General_______
 A. This procedure contains the tasks that follow:
 (1)  
The removal of the wing landing gear from the airplane

 (2)  
The installation of the wing landing gear on the airplane.

 B.
The airplane must be on jacks to do the tasks that are in this procedure.


 TASK 32-11-01-004-001
 2.  Wing Landing Gear Removal (Fig. 401 and 402)_________________________
 A. Special Tools and Equipment
 (1)  
8ME65B00161-1 - Drag Brace Support Strap

 (2)  
8ME65B01202-3 - Wing Gear Oleo Lock Assembly

 (3)  
G32028-116 - Wing Gear Oleo Jack (Preferred , applicable to all Airplanes)

 (4)  
G32028-141 Wing Gear Oleo Jack (Optional, applicable to only Airplanes with wing landing gear Outer Cylinder Gland Nut Lock Tabs facing forward)

 (5)  
G32028-117 Wing Gear Oleo Jack (Optional, applicable to only Airplanes with wing landing gear Outer Cylinder Gland Nut Lock Tabs facing inboard)

 B.
Standard Tools and Equipment

 (1)  
Inclinometer

 (2)  
Axle jacks with adapters - 4000-pound capacity (2 required)
 
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